As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIA 0.709", FINAL HOLE DIA 0.738", MAXIMUM ALLOWABLE HOLE DIA 0.709". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0340973 PART 1 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.